Wireless spread spectrum ground link-based aircraft data communication system with variable data rate

• US 6,163,681 A
• Filed: 06/25/1999
• Issued: 12/19/2000
• Est. Priority Date: 06/25/1999
• Status: Expired due to Term

• Current Assignee: Harris Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Harris Corporation (L3Harris Technologies, Inc.)
• Inventors: Wright, Thomas H., Salati, Bruce D.
• Primary Examiner(s): Crosland, Donnie L.
• Application Number:
  US09/340,003
• Time in Patent Office: 543 Days
• Field of Search: 455/66, 455/73, 455/431, 455/67.1, 701/3, 701/13, 701/14, 701/29, 701/35, 340/945, 340/961, 340/971, 340/825.15, 340/825.16, 340/825.69, 340/825.72, 375/200, 375/219, 375/220
• US Class Current: 455/66.1
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service

Abstract

A system and method of the present invention exchanges information to and from an aircraft and includes a ground data link unit and a data store, which accumulates and stores data files that have been uploaded to the aircraft, and flight performance data related to flight performance of the aircraft in flight. A spread spectrum transceiver of the ground data link unit is operative at a first higher data rate when the aircraft is on the ground, and a second substantially lower data rate when the aircraft is airborne in close proximity to the airport and downloads the flight performance data and uploads other data to and from an airport base spread spectrum transceiver.

Claims

1. A system for exchanging information to and from an aircraft comprising:

a ground data link unit that obtains data during flight of the aircraft, said ground data link unit comprising;

a) a data store operative to accumulate and store data files that have been uploaded to the aircraft and flight performance data related to the flight performance of the aircraft in flight;

b) a spread spectrum transceiver coupled to said data store that is operative at a first higher data rate when the aircraft is on the ground and a second substantially lower, data rate when the aircraft is airborne in close proximity to the airport to increase effective communication range, wherein said spread spectrum transceiver further comprises a transmitter for downloading said data files that have been uploaded to the aircraft and flight performance data that has been accumulated and stored by said data store over a spread spectrum communication signal, and a receiver for uploading data over a second spread spectrum communication signal; and

an airport based spread spectrum transceiver that is operative to transmit and receive data to and from said aircraft ground data link unit along respective first and second spread spectrum communication signals at a first data rate when the aircraft is on the ground and a second data rate when the aircraft is airborne in proximity to the airport.

2. A system according to claim 1, wherein said flight performance data includes data relating to fuel consumption and maintenance requirements to enhance aircraft service at a landing gate.

3. A system according to claim 1, wherein said airport based spread spectrum transceiver and said spread spectrum transceiver on said aircraft further comprise omnidirectional antenna used on the ground to provide gain.

4. A system according to claim 1, wherein said spread spectrum communication signal is chosen to have a frequency in a band that is below the resonant frequency of oxygen and water molecules in order to minimize the effects of atmospheric absorption loss and rain fading on communication range.

5. A system according to claim 1, wherein said aircraft further comprises an antenna that is elevated to aid in eliminating ground multipath.

6. A system according to claim 1, wherein said spread spectrum transceivers include frequency oscillators having sufficient frequency stability coupled with carrier tracking loops with sufficient bandwidth to track out frequency uncertainty caused by Doppler frequency shift.

7. A system according to claim 1, wherein said flight performance data includes engine data obtained from an aircraft engine concerning operation of the engine.

8. A system according to claim 1, wherein said spread spectrum transceiver further comprises narrow band baseband filters that are operative at the second, substantially lower data rate.

9. A system according to claim 1, wherein said first, higher data is about 1 Mbps to about 11 Mbps and said second, substantially lower data rate is about 300 Kbps to about 1 Mbps.

10. A system according to claim 1, and further comprising an airport based archival data store coupled to said airport based spread spectrum receiver that receives and stores said flight performance data that has been downloaded to the airport based spread spectrum transceiver.

11. A system according to claim 10, and further comprising a wireless router that couples said airport based spread spectrum receiver to said airport based archival data store.

12. A system according to claim 1, and further comprising a ground based server coupled to said airport based spread spectrum receiver for receiving flight performance data from the airport based spread spectrum receiver.

13. A system according to claim 1, and further comprising a remote flight operations control center operatively coupled to said ground based server for retrieving and processing the flight performance data.

14. A system according to claim 1, wherein the spread spectrum communication signal comprises a direct sequence spread spectrum signal.

15. A system according to claim 1, wherein the spread spectrum communication signal comprises a signal within the S band.

16. A system according to claim 1, wherein the spread spectrum communication signal comprises a signal within the range of about 2.4 to about 2.5 GHz.

17. A system according to claim 1, wherein said data store of said ground data link unit further comprises means for compressing said flight performance data during the flight of the aircraft.

18. A system for providing a retrievable record of the flight performance of an aircraft comprising:

a ground data link unit that obtains flight performance data representative of aircraft flight performance during flight of the aircraft, said ground data link unit comprising;

a) a data store operative to accumulate and store flight performance data relating to the performance of the aircraft during flight of the aircraft, and

b) a spread spectrum transceiver coupled to said data store, and comprising a transmitter that is operative after the aircraft completes its flight and lands at an airport to download said flight performance data that has been accumulated and stored by said data store during flight over a spread spectrum communication signal at a first, higher data rate, and wherein said spread spectrum transceiver is operative to download flight performance data at a second, substantially lower data rate when the aircraft is in flight and in close proximity to the airport; and

an airport based spread spectrum receiver that receives the spread spectrum communication signal from the aircraft and demodulates the signal to obtain the flight performance data.

19. A system according to claim 18, wherein said flight performance data includes data relating to fuel consumption and maintenance requirements to enhance aircraft service at a landing gate.

20. A system according to claim 18, wherein said airport based spread spectrum transceiver and said spread spectrum transceiver on said aircraft further comprise omnidirectional antenna used on the ground to provide gain.

21. A system according to claim 18, wherein said spread spectrum communication signal is chosen to have a frequency in a band that is below the resonant frequency of oxygen and water molecules in order to minimize the effects of atmospheric absorption loss and rain fading on communication range.

22. A system according to claim 18, wherein said aircraft further comprises an antenna that is elevated to aid in eliminating ground multipath.

23. A system according to claim 18, wherein said spread spectrum transceivers include frequency oscillators having sufficient frequency stability coupled with carrier tracking loops with sufficient bandwidth to track out frequency uncertainty caused by Doppler frequency shift.

24. A system according to claim 18, wherein said flight performance data includes engine data obtained from an aircraft engine concerning the operation of the engine.

25. A system according to claim 18, wherein said spread spectrum transceiver further comprises narrow band baseband filters that are operative at the second, substantially lower data rate.

26. A system according to claim 18, wherein said first higher data is about 1 Mbps to about 11 Mbps and said second, substantially lower data rate is about 300 Kbps to about 1 Mbps.

27. A system according to claim 18, and further comprising an airport based archival data store coupled to said airport based spread spectrum receiver that receives and stores said flight performance data that has been downloaded to the airport based spread spectrum transceiver.

28. A system according to claim 27, and further comprising a wireless router that couples said airport based spread spectrum receiver to said airport based archival data store.

29. A system according to claim 18, and further comprising a ground based server coupled to said airport based spread spectrum receiver for receiving flight performance data from the airport based spread spectrum receiver.

30. A system according to claim 29, and further comprising a remote flight operations control center operatively coupled to said ground based server for retrieving and processing the flight performance data.

31. A system according to claim 18, wherein the spread spectrum communication signal comprises a direct sequence spread spectrum signal.

32. A system according to claim 18, wherein the spread spectrum communication signal comprises a signal within the S band.

33. A system according to claim 18, wherein the spread spectrum communication signal comprises a signal within the range of about 2.4 to about 2.5 GHz.

34. A system according to claim 18, wherein said archival data store of said ground data link unit further comprises means for compressing said flight performance data during the flight of the aircraft.

35. A method for exchanging information to and from an aircraft comprising the steps of:

collecting data within a ground data link unit on the flight performance of the aircraft during flight of the aircraft and data files that have been uploaded;

accumulating and storing within a data store the flight performance data and buffering data files that have been uploaded during flight of the aircraft;

downloading to an airport based spread spectrum transceiver the flight performance data that has been accumulated and stored during flight and buffered data files over a spread spectrum communication signal at a first higher data rate when the aircraft is on the ground, and a second, substantially lower data rate when the aircraft is airborne in close proximity to the airport;

demodulating the received spread spectrum communication signal to obtain the flight performance data;

uploading data files from the airport based spread spectrum transceiver along a second spread spectrum communication signal to a spread spectrum transceiver of the ground data link at the first higher data rate when the aircraft is on the ground and at a second, substantially lower data rate when the aircraft is airborne in close proximity to the airport; and

demodulating the received spread spectrum communication signal within the spread spectrum transceiver of the ground data link unit.

36. A method according to claim 35, and further comprising the step of storing the uploaded files after demodulation within the data store of the ground data link unit on the aircraft.

37. A method according to claim 35, wherein the flight performance data comprises data relating to fuel consumption and maintenance requirements.

38. A method according to claim 35, and further comprising the step of downloading flight performance data relating to fuel consumption and maintenance requirements at the second, substantially lower data rate as the aircraft approaches in close proximity to the airport.

39. A method according to claim 35, wherein the flight performance data comprises engine data obtained from the aircraft engine concerning operation of the engine.

40. A method according to claim 35, and further comprising the step of passing the spread spectrum communication signal at the second, substantially lower data rate through narrow band baseband filters to improve signal-to-noise ratio.

41. A method according to claim 35, wherein the first higher data rate is about 1 Mbps to about 11 Mbps and the second, lower data rate is about 300 Kbps to about 1 Mbps.

42. A method according to claim 35, and further comprising the step of receiving and storing the flight performance data that has been downloaded to the airport based spread spectrum transceiver within an airport based archival data store.

43. A method according to claim 35, and further comprising the step of forwarding the demodulated spread spectrum communication signal from the airport based spread spectrum transceiver to an airport based archival data store via a wireless router.

44. A method according to claim 35, and further comprising the step of forwarding the demodulated spread spectrum communication signal from the airport based spread spectrum transceiver to a ground based server for further processing.

45. A method according to claim 44, and further comprising the step of forwarding the demodulated spread spectrum communication signal from the ground based server to a remote flight operations control center.

46. A method according to claim 35, wherein the spread spectrum communication signal comprises a direct sequence spread spectrum signal.

47. A method according to claim 35, wherein the spread spectrum communication signal comprises a signal within the S band.

48. A method according to claim 35, wherein the spread spectrum communication signal comprises a signal within the range of about 2.4 to about 2.5 GHz.

49. A method according to claim 35, and further comprising the step of compressing the flight performance data within the archival memory storage during flight of the aircraft.

50. A method according to claim 35, and further comprising the step of transmitting and receiving in a frequency band that is below the resonant frequency of oxygen and water molecules in order to minimize the effects of atmospheric absorption loss and rain fading on the communication range.

51. A method according to claim 35, and further comprising the step of transmitting and receiving with spread spectrum transceivers having frequency oscillators having sufficient frequency stability coupled with carrier tracking loops with sufficient bandwidth to track out frequency uncertainty caused by Doppler frequency shift.

52. A ground data link unit that obtains flight performance data representative of aircraft flight performance during flight of the aircraft, said ground data link unit comprising:

a data store operative to accumulate and store data files that have been uploaded to the aircraft and flight performance data related to the flight performance of the aircraft in flight; and

a spread spectrum transceiver coupled to said data store that is operative at a first higher data rate when the aircraft is on the ground and a second substantially lower, data rate when the aircraft is airborne in close proximity to the airport to increase effective communication range, wherein said spread spectrum transceiver further comprises a transmitter for downloading said flight performance data that has been accumulated and stored by said data store over a spread spectrum communication signal, and a receiver for uploading data over a second spread spectrum communication signal.

53. A ground data link unit according to claim 52, wherein said flight performance data includes data relating to fuel consumption and maintenance requirements to enhance aircraft service at a landing gate.

54. A ground data link unit according to claim 52, wherein said airport based spread spectrum transceiver and said spread spectrum transceiver on said aircraft further comprise omnidirectional antenna used on the ground to provide gain.

55. A system according to claim 52, wherein said spread spectrum communication signal is chosen to have a frequency in a band that is below the resonant frequency of oxygen and water molecules in order to minimize the effects of atmospheric absorption loss and rain fading on communication range.

56. A system according to claim 52, wherein said aircraft further comprises an antenna that is elevated to aid in eliminating ground multipath.

57. A system according to claim 52, wherein said spread spectrum transceivers include frequency oscillators having sufficient frequency stability coupled with carrier tracking loops with sufficient bandwidth to track out frequency uncertainty caused by Doppler frequency shift.

58. A system according to claim 52, wherein said flight performance data includes engine data obtained from an aircraft engine concerning operation of the engine.